New Dynamic Stability Rig for Tri-sonic Wind-Tunnel

摘要：

　　The present-day unconventional and high-lifting aerospace configuration design has greatly increased the demand for accurate prediction and expanded measure dynamic stability derivatives envelopes of conventional aerospace vehicles.With these issues in mind,china academy of aerospace aerodynamics(CAAA)designed and built a forced oscillation test rig in the sub-,tran-and supersonic wind tunnel that provides new capabilities for aerodynamic researchers to accurately measure the dynamic derivatives and investigate the asymmetric coupling effects of high-lifting aerospace configuration vehicles.

关键词： unconventional and high-lifting aerospace vehicles forced oscillation rig the asymmetric coupling effects tri-sonic wind tunnel

作者: Liu Jin Chen Nong Song Yuhui Hu Jing Cheng Lan Wang Fangjian

作者单位: China Academy of Aerospace Aerodynamics,Beijing 100074,China

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-5

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）